View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 43131U 18004W 23095.98295447 .12392626 24865-5 90540-3 0 9994
2 43131 97.3029 186.4918 0014837 270.8730 89.0869 16.39617505291893
| Epoch (UTC): | 05 April 2023 23:35:27 |
| Eccentricity: | 0.0014837 |
| inclination: | 97.3029° |
| perigee height: | 157 km |
| apogee height: | 176 km |
| right ascension of ascending node: | 186.4918° |
| argument of perigee: | 270.8730° |
| revolutions per day: | 16.39617505 |
| mean anomaly at epoch: | 89.0869° |
| orbit number at epoch: | 29189 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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